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US 2024/0359809 A1Published application
Fuel tank for an aircraft, fuselage of an aircraft, and aircraft
OwnerPeter LINDE, Michael TELKAMPinventors
Life of this patent
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Abstract
A tank for an aircraft, the tank comprising two pressure bulkheads which are connected to each other by a tank wall which is at least partially formed by a portion of a skin of the aircraft's fuselage. The tank further comprises at least one anti-sloshing wall at least partially enclosing one or several openings and at least partially formed by a belonging frame stabilizing the skin. Also a fuselage with such tank, and an aircraft with such fuselage.
Claims11
A fuel tank for an aircraft, the fuel tank comprising:
- two pressure bulkheads which are connected to each other by a tank wall at least partially formed by a portion of a skin of a fuselage of the aircraft;
- and,
- at least one anti-sloshing wall at least partially enclosing one or more openings and at least partially formed by a belonging frame stabilizing said skin.
Dependencies are inferred from the claim text.